WE54A Magnesium vs. 242.0 Aluminum
WE54A magnesium belongs to the magnesium alloys classification, while 242.0 aluminum belongs to the aluminum alloys. There are 32 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown.
For each property being compared, the top bar is WE54A magnesium and the bottom bar is 242.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 85 | |
| 70 to 110 |
| Elastic (Young's, Tensile) Modulus, GPa | 44 | |
| 73 |
| Elongation at Break, % | 4.3 to 5.6 | |
| 0.5 to 1.5 |
| Fatigue Strength, MPa | 98 to 130 | |
| 55 to 110 |
| Poisson's Ratio | 0.29 | |
| 0.33 |
| Shear Modulus, GPa | 17 | |
| 27 |
| Shear Strength, MPa | 150 to 170 | |
| 150 to 240 |
| Tensile Strength: Ultimate (UTS), MPa | 270 to 300 | |
| 180 to 290 |
| Tensile Strength: Yield (Proof), MPa | 180 | |
| 120 to 220 |
Thermal Properties
| Latent Heat of Fusion, J/g | 330 | |
| 390 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 210 |
| Melting Completion (Liquidus), °C | 640 | |
| 640 |
| Melting Onset (Solidus), °C | 570 | |
| 530 |
| Solidification (Pattern Maker's) Shrinkage, % | 1.6 | |
| 1.3 |
| Specific Heat Capacity, J/kg-K | 960 | |
| 870 |
| Thermal Conductivity, W/m-K | 52 | |
| 130 to 170 |
| Thermal Expansion, µm/m-K | 25 | |
| 22 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 10 | |
| 33 to 44 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 47 | |
| 96 to 130 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 34 | |
| 12 |
| Density, g/cm3 | 1.9 | |
| 3.1 |
| Embodied Carbon, kg CO2/kg material | 29 | |
| 8.3 |
| Embodied Energy, MJ/kg | 260 | |
| 150 |
| Embodied Water, L/kg | 900 | |
| 1130 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 10 to 14 | |
| 1.3 to 3.4 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 360 to 380 | |
| 110 to 340 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 62 | |
| 45 |
| Strength to Weight: Axial, points | 39 to 43 | |
| 16 to 26 |
| Strength to Weight: Bending, points | 49 to 51 | |
| 23 to 32 |
| Thermal Diffusivity, mm2/s | 28 | |
| 50 to 62 |
| Thermal Shock Resistance, points | 18 to 19 | |
| 8.0 to 13 |
Alloy Composition
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| Aluminum (Al), % | 0 | |
| 88.4 to 93.6 |
| Chromium (Cr), % | 0 | |
| 0 to 0.25 |
| Copper (Cu), % | 0 to 0.030 | |
| 3.5 to 4.5 |
| Iron (Fe), % | 0 to 0.010 | |
| 0 to 1.0 |
| Lithium (Li), % | 0 to 0.2 | |
| 0 |
| Magnesium (Mg), % | 88.7 to 93.4 | |
| 1.2 to 1.8 |
| Manganese (Mn), % | 0 to 0.030 | |
| 0 to 0.35 |
| Nickel (Ni), % | 0 to 0.0050 | |
| 1.7 to 2.3 |
| Silicon (Si), % | 0 to 0.010 | |
| 0 to 0.7 |
| Titanium (Ti), % | 0 | |
| 0 to 0.25 |
| Unspecified Rare Earths, % | 1.5 to 4.0 | |
| 0 |
| Yttrium (Y), % | 4.8 to 5.5 | |
| 0 |
| Zinc (Zn), % | 0 to 0.2 | |
| 0 to 0.35 |
| Zirconium (Zr), % | 0.4 to 1.0 | |
| 0 |
| Residuals, % | 0 to 0.3 | |
| 0 to 0.15 |